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Nonlinear Analysis and Synthesis Techniques for Aircraft Control 2007th Edition by Declan Bates, Martin Hagstrom ISBN 3540737189 9783540737186

  • SKU: BELL-2120258
Nonlinear Analysis and Synthesis Techniques for Aircraft Control 2007th Edition by Declan Bates, Martin Hagstrom ISBN 3540737189 9783540737186
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Nonlinear Analysis and Synthesis Techniques for Aircraft Control 2007th Edition by Declan Bates, Martin Hagstrom ISBN 3540737189 9783540737186 instant download after payment.

Publisher: Springer
File Extension: PDF
File size: 6.54 MB
Pages: 367
Author: Declan Bates, Martin Hagstrom
ISBN: 9783540737186, 3540737189
Language: English
Year: 2007
Edition: 1

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Nonlinear Analysis and Synthesis Techniques for Aircraft Control 2007th Edition by Declan Bates, Martin Hagstrom ISBN 3540737189 9783540737186 by Declan Bates, Martin Hagstrom 9783540737186, 3540737189 instant download after payment.

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ISBN 10: 3540737189 
ISBN 13: 9783540737186
Author: Declan Bates, Martin Hagstrom

Despite many signi?cant advances in the theory of nonlinear control in recent years, the majority of control laws implemented in the European aerospace - dustry are still designed and analysed using predominantly linear techniques applied to linearised models of the aircrafts’ dynamics. Given the continuous increase in the complexity of aircraft control laws, and the corresponding - crease in the demands on their performance and reliability, industrial control law designers are highly motivated to explore the applicability of new and more powerful methods for design and analysis. The successful application of fully nonlinear control techniques to aircraft control problems o?ers the prospect of improvements in several di?erent areas. Firstly, there is the possibility of - proving design and analysis criteria to more fully re?ect the nonlinear nature of the dynamics of the aircraft. Secondly, the time and e?ort required on the part of designers to meet demanding speci?cations on aircraft performance and h- dling could be reduced. Thirdly, nonlinear analysis techniques could potentially reduce the time and resources required to clear ?ight control laws, and help to bridge the gap between design, analysis and ?nal ?ight clearance. Theaboveconsiderationsmotivatedtheresearchpresentedinthisbook,which is the result of a three-year research e?ort organised by the Group for Aeron- tical Research and Technology in Europe (GARTEUR). In September 2004, GARTEUR Flight Mechanics Action Group 17 (FM-AG17) was established to conduct research on ”New Analysis and Synthesis Techniques for Aircraft Control”.

Nonlinear Analysis and Synthesis Techniques for Aircraft Control 2007th Table of contents:

Part I: Nonlinear Analysis Techniques for Aircraft Control

  1. Tools and Methods for Nonlinear System Analysis
    • Phase Plane Analysis (for lower-order systems)
    • Lyapunov Stability Theory (Direct and Indirect Methods)
    • Input-to-State Stability (ISS)
    • Describing Function Method
    • Bifurcation Analysis (e.g., limit cycles, stability boundaries)
    • Sum-of-Squares (SOS) Programming for Nonlinear Analysis (as a more modern technique)
  2. Nonlinear Aircraft Models
    • High-Fidelity Nonlinear Aircraft Dynamics (longitudinal, lateral-directional)
    • Aerodynamic Nonlinearities (high angle of attack, stall/post-stall)
    • Actuator Dynamics and Limitations (rate and position limits, saturations)
    • Aeroelastic Effects and Freeplay (if discussed)
  3. Analysis of Existing Aircraft Control Systems
    • Assessing Nonlinear Behavior of Gain-Scheduled Controllers
    • Robustness Analysis of Nonlinear Systems (e.g., μ-analysis, structured singular values for nonlinearities)
    • Analysis of Limit Cycle Oscillations and Flight Envelope Boundaries

Part II: Nonlinear Synthesis Techniques for Aircraft Control

  1. Nonlinear Control Design Methodologies
    • Feedback Linearization:
      • Exact/Approximate Feedback Linearization
      • Dynamic Inversion Control
    • Sliding Mode Control (SMC):
      • Basic Principles and Design
      • Chattering Reduction Techniques
    • Backstepping Control:
      • Recursive Design for Cascaded Systems
    • Nonlinear Model Predictive Control (NMPC):
      • Principles and Application to Aircraft
    • Adaptive Nonlinear Control:
      • Handling Uncertainties and Unknown Dynamics
    • Fuzzy Logic and Neural Network Control (if included, often as intelligent control)
    • LMI-based Control Synthesis (for robust nonlinear control)
  2. Application to Flight Control Problems
    • Full Flight Envelope Control:
      • Control Beyond Stall/High Angle of Attack
      • Aggressive Maneuvering Control
    • Reconfigurable Flight Control:
      • Control in the Presence of Faults or Damage
    • Thrust Vectoring Control
    • UAV/UCAV Control (if discussed, given its relevance to nonlinear dynamics)

Part III: Specific Applications and Case Studies (Often a major focus in such books)

  1. On-Ground Aircraft Control
    • Speed Control:
      • Braking Control Systems
      • Engine Thrust Control for Taxiing
    • Directional Control:
      • Nose Wheel Steering Systems (nonlinearities and saturation)
      • Thrust Reverser/Differential Braking for Directional Control
      • Integrated Control for Take-off and Landing
  2. Control of Specific Aircraft Subsystems with Nonlinearities
    • Landing Gear Dynamics and Control
    • Braking Systems with Antiskid Control
    • Actuator Nonlinearities and Compensation
  3. Fault Tolerant Control in Nonlinear Aircraft Systems
    • Detection, Isolation, and Accommodation of Faults
    • Using Nonlinear Control for Reconfiguration

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Tags: Declan Bates, Martin Hagstrom, Nonlinear

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